EP2752291A1 - Tôle métallique revêtue de résine - Google Patents

Tôle métallique revêtue de résine Download PDF

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Publication number
EP2752291A1
EP2752291A1 EP11871436.9A EP11871436A EP2752291A1 EP 2752291 A1 EP2752291 A1 EP 2752291A1 EP 11871436 A EP11871436 A EP 11871436A EP 2752291 A1 EP2752291 A1 EP 2752291A1
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EP
European Patent Office
Prior art keywords
resin coating
metal sheet
resin
coating layer
less
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP11871436.9A
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German (de)
English (en)
Other versions
EP2752291B1 (fr
EP2752291A4 (fr
Inventor
Junichi Kitagawa
Yoichiro Yamanaka
Yusuke Nakagawa
Katsumi Kojima
Mikito Suto
Yoichi Tobiyama
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
JFE Steel Corp
Original Assignee
JFE Steel Corp
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Publication date
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Publication of EP2752291A1 publication Critical patent/EP2752291A1/fr
Publication of EP2752291A4 publication Critical patent/EP2752291A4/fr
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Publication of EP2752291B1 publication Critical patent/EP2752291B1/fr
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B1/00—Layered products having a general shape other than plane
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • B32B15/09—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin comprising polyesters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B27/08—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/18—Layered products comprising a layer of synthetic resin characterised by the use of special additives
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/18—Layered products comprising a layer of synthetic resin characterised by the use of special additives
    • B32B27/20—Layered products comprising a layer of synthetic resin characterised by the use of special additives using fillers, pigments, thixotroping agents
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/36—Layered products comprising a layer of synthetic resin comprising polyesters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00—Layers arrangement
    • B32B2250/03—3 layers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2250/00—Layers arrangement
    • B32B2250/05—5 or more layers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2255/00—Coating on the layer surface
    • B32B2255/10—Coating on the layer surface on synthetic resin layer or on natural or synthetic rubber layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/30—Properties of the layers or laminate having particular thermal properties
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/70—Other properties
    • B32B2307/702—Amorphous
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/70—Other properties
    • B32B2307/746—Slipping, anti-blocking, low friction
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2311/00—Metals, their alloys or their compounds
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2367/00—Polyesters, e.g. PET, i.e. polyethylene terephthalate
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2391/00—Waxes
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00—Use of inorganic substances as compounding ingredients
    • C08K3/18—Oxygen-containing compounds, e.g. metal carbonyls
    • C08K3/20—Oxides; Hydroxides
    • C08K3/22—Oxides; Hydroxides of metals
    • C08K2003/2237—Oxides; Hydroxides of metals of titanium
    • C08K2003/2241—Titanium dioxide
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00—Use of inorganic substances as compounding ingredients
    • C08K3/01—Use of inorganic substances as compounding ingredients characterized by their specific function
    • C08K3/013—Fillers, pigments or reinforcing additives
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L67/00—Compositions of polyesters obtained by reactions forming a carboxylic ester link in the main chain; Compositions of derivatives of such polymers
    • C08L67/02—Polyesters derived from dicarboxylic acids and dihydroxy compounds
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L67/00—Compositions of polyesters obtained by reactions forming a carboxylic ester link in the main chain; Compositions of derivatives of such polymers
    • C08L67/02—Polyesters derived from dicarboxylic acids and dihydroxy compounds
    • C08L67/03—Polyesters derived from dicarboxylic acids and dihydroxy compounds the dicarboxylic acids and dihydroxy compounds having the carboxyl- and the hydroxy groups directly linked to aromatic rings
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L91/00—Compositions of oils, fats or waxes; Compositions of derivatives thereof
    • C08L91/06—Waxes
    • C—CHEMISTRY; METALLURGY
    • C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09D—COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
    • C09D191/00—Coating compositions based on oils, fats or waxes; Coating compositions based on derivatives thereof
    • C09D191/06—Waxes
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
    • Y10T428/263—Coating layer not in excess of 5 mils thick or equivalent
    • Y10T428/264—Up to 3 mils
    • Y10T428/265—1 mil or less
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31678—Of metal
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31678—Of metal
    • Y10T428/31681—Next to polyester, polyamide or polyimide [e.g., alkyd, glue, or nylon, etc.]
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31786—Of polyester [e.g., alkyd, etc.]
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/31504—Composite [nonstructural laminate]
    • Y10T428/31801—Of wax or waxy material

Definitions

  • the present invention relates to a resin coated metal sheet in which a metal sheet has resin coating layers on both sides thereof.
  • metal containers are broadly divided into two-piece cans and three-piece cans.
  • the two-piece can refers to a metal container consisting of two parts of a can body integral with a can bottom and a lid body.
  • the three-piece can refers to a metal container consisting of three parts of a can barrel, an upper lid, and a bottom lid.
  • the can body of the two-piece can has fine appearance because it has no seamed part (welded part), it in general requires a high degree of working.
  • the can barrel of the three-piece can is inferior in appearance as compared to the can body of the two-piece can because it has seamed parts, it does not in general require a high degree of working. Given these circumstances, there is a tendency that the two-piece cans are used for expensive small-volume metal containers and the three-piece cans are used for inexpensive large-volume metal containers.
  • a metal material for a can body of a two-piece can that has a high degree of working in drawing and has a high degree of stretching in a can height direction that is, a two-piece can having a high degree of working
  • a soft metal material such as aluminum, which is expensive and has a large sheet thickness
  • a steel sheet such as tinplate or tin-free steel, which is inexpensive and has a small sheet thickness, is little used.
  • the impact forming method having a high degree of working such as the drawing method and the draw and ironing (DI) method are hard to be adopted to the steel sheet, the impact forming method having a high degree of working can be applied to the soft metal material.
  • the two-piece can having a high degree of working include an aerosol can.
  • Patent Literature 1 to 3 For a two-piece can having a low degree of working, technologies have been developed for manufacturing can bodies by the drawing method and the DI method using as a material a resin coated metal sheet in which a metal sheet has resin coating layers on both sides thereof. In order to allow treatment for improving the designability of a can body such as printing treatment, technologies have also been developed for adding a white pigment to a resin coating layer positioned outside a metal container after forming (see Patent Literature 4 and 5).
  • the inventors of the present invention considered that if a can body of a two-piece can having a high degree of working can be manufactured using a steel sheet that is inexpensive and has high strength despite of its small sheet thickness, a two-piece can having a high degree of working can be provided at a lower price.
  • the inventors then manufactured a can body of a two-piece can having a high degree of working using a resin coated metal sheet and performed heat treatment at a temperature close to the melting point of the resin coating layer in order to increase adhesion between the resin coating layer and a metal sheet after forming, the laminatability of the back side resin coating layer positioned inside a metal container after forming, and the designability of the front side resin coating layer positioned outside the metal container after forming.
  • the present invention has been achieved in view of the above circumstances, and an object thereof is to provide a resin coated metal sheet in which no appearance defect (surface roughness) is caused by heat treatment.
  • the inventors of the present invention found that the appearance defects are caused by heat treatment because a residual stress within the resin coating layer that has developed during forming is relaxed by heat treatment and the resin coating layer becomes deformed unevenly to form uneven distribution of a pigment. Based on this finding, the inventors of the present invention made further study to achieve a technical idea that the residual stress of the resin coating layer after forming can be reduced by controlling the degree of crystallinity of the resin coating layer, thereby reducing the uneven deformation of the resin coating layer and the occurrence of appearance defects caused by heat treatment.
  • a resin coated metal sheet according to the present invention includes: resin coating layers on both sides of a metal sheet, wherein one of the resin coating layers that is positioned outside a container after forming is formed of a resin material whose difference between a heat quantity of crystallization and a heat quantity of fusion after being laminated to the metal sheet is within a range of 0 J/g or more and 20 J/g or less on a unit weight basis.
  • the resin coated metal sheet according to the present invention can reduce the residual stress of the resin coating layer positioned outside a container after forming, thereby reducing the occurrence of appearance defects caused by heat treatment.
  • FIG. 1 is a sectional view illustrating the constitution of the resin coated metal sheet according to the embodiment of the present invention.
  • FIG. 2 is a sectional view illustrating the constitution of a modification to the resin coated metal sheet illustrated in FIG. 1 .
  • this resin coated metal sheet 1 according to the embodiment of the present invention includes a metal sheet 2, a resin coating layer 3 formed on the front side of the metal sheet 2, and a resin coating layer 4 formed on the back side of the metal sheet 2.
  • the resin coating layer 3 and the resin coating layer 4 are positioned outside and inside a metal container after forming, respectively.
  • the metal sheet 2 is formed of a steel sheet such as tinplate or tin-free steel.
  • tinplate one having a plating amount of 0.5 to 15 g/m 2 may be used.
  • the tin-free steel may have on its surface a chromium metal layer with an adhesion amount of 50 to 200 mg/m 2 and a chromium oxide layer with an adhesion amount of 3 to 30 mg/m 2 on a chromium metal layer basis.
  • the steel sheet which is not limited in particular in its type, so long as it can be formed into an intended shape, is preferably one based on the following components and manufacturing methods.
  • the mechanical property of the steel sheet is not limited in particular so long as the steel sheet can be formed into an intended shape, but in order not to impair workability and to maintain sufficient can body strength, a steel sheet whose yield strength YP is about 220 MPa or more and 580 MPa or less is preferably used.
  • a steel sheet whose yield strength YP is about 220 MPa or more and 580 MPa or less is preferably used.
  • the Lankford (r-value) as an indicator of plastic anisotropy one with a value of 0.8 or more is preferable
  • the intra-plane anisotropy ⁇ r of the r-value one with its absolute value of 0.7 or less is preferable.
  • the sheet thickness of the steel sheet can be appropriately set based on the shape of an intended can and necessary can body strength. In view of reducing an increase in the cost of the steel sheet and the can body, a steel sheet with a sheet thickness of about 0.15 to 0.4 mm is preferably used.
  • the resin coating layers 3 and 4 are formed of a resin material containing 90 mol% or more ethylene terephthalate unit, preferably 92 mol% or more.
  • a resin material with ethylene terephthalate unit being less than 90 mol% is not preferable, because the resin material is subjected to heat treatment at nearly the melting point after forming, which causes thermal degradation. Without impairing its heat resistance and workability, the resin material may be copolymerized with other components such as a dicarboxylic acid component and a glycol component.
  • dicarboxylic acid examples include: aromatic dicarboxylic acids such as isophthalic acid, naphthalene dicarboxylic acid, diphenyl dicarboxylic acid, diphenyl sulfone dicarboxylic acid, diphenoxyethane dicarboxylic acid, 5-sodium sulfoisophthalic acid, and phthalic acid; aliphatic dicarboxylic acids such as oxalic acid, succinic acid, adipic acid, sebacic acid, dimer acid, maleic acid, and fumaric acid; alicyclic dicarboxylic acid such as cyclohexane dicarboxylic acid; and oxycarboxylic acid such as p-oxybenzoic acid.
  • aromatic dicarboxylic acids such as isophthalic acid, naphthalene dicarboxylic acid, diphenyl dicarboxylic acid, diphenyl sulfone dicarboxylic acid, diphenoxyethan
  • glycol component examples include: aliphatic glycols such as propanediol, butanediol, pentanediol, hexanediol, and neopentyl glycol; alicyclic glycol such as cyclohexane dimethanol; aromatic glycols such as bisphenol A and bisphenol S; and diethylene glycol. Two or more of these dicarboxylic acid components and the glycol components may be used in combination.
  • aliphatic glycols such as propanediol, butanediol, pentanediol, hexanediol, and neopentyl glycol
  • alicyclic glycol such as cyclohexane dimethanol
  • aromatic glycols such as bisphenol A and bisphenol S
  • diethylene glycol Two or more of these dicarboxylic acid components and the glycol components may be used in combination.
  • the resin material forming the resin coating layers 3 and 4 is not limited in its manufacturing method.
  • the resin material can be manufactured by, for example, (1) a method in which terephthalic acid, ethylene glycol, and a copolymerization component are subjected to an esterification reaction, and then the resultant reaction product is polycondensed to obtain copolyester and (2) a method in which dimethyl terephthalate, ethylene glycol, and a copolymerization component are subjected to a transesterification reaction, and then the resultant reaction product is polycondensed to obtain copolyester.
  • additives such as fluorescent brightening agents, antioxidants, thermal stabilizers, UV absorbers, and antistatic agents may be added as needed. The addition of a fluorescent brightening agent is effective in improving whiteness.
  • the time period during which the resin coating layers 3 and 4 are held at a temperature of not less than their melting point during lamination to the metal sheet 2 is preferably within a range of 1 to 30 milliseconds.
  • Pressing pressure during the lamination is not limited in particular, but the surface pressure is preferably within a range of 9.8 to 294 N (1 to 30 kgf/cm 2 ).
  • the surface pressure is lower than this range, even when the temperature of the boundary surface between the metal sheet 2 and the resin coating layers 3 and 4 is not less than the melting point, the resin coating layers 3 and 4 melt insufficiently, because the time period during which the temperature is not less than the melting point is short, which may fail to achieve sufficient adhesion between the resin coating layers 3 and 4 and the metal sheet 2.
  • the surface pressure is higher than this range, the deposition of the resin coating layers 3 and 4 may occur.
  • Melt extrusion lamination may be applied in which a melted resin material, instead of the film-like resin material, is laminated to the surface of the metal sheet 2.
  • the resin coating layer 3 is formed of a resin material whose difference between the heat quantity of crystallization and the heat quantity of fusion after being laminated to the metal sheet 2 is within a range of 0 J/g or more and 20 J/g or less, preferably 0 J/g or more and 18 J/g or less, and more preferably 0 J/g 14 J/g or less, on a unit weight basis.
  • the heat quantity of crystallization and the heat quantity of fusion can be measured using a differential scanning calorimetry (DSC). The difference between the heat quantity of crystallization and the heat quantity of fusion gives an indicator of the degree of crystallinity of the resin coating layer 3 after lamination.
  • the resin coating layer 3 When the difference between the heat quantity of crystallization and the heat quantity of fusion is 0 J/g, the resin coating layer 3 is in an amorphous state, the degree of crystallinity of the resin coating layer 3 is nearly zero, and a residual stress after forming is low. For this reason, no appearance defect is caused by heat treatment.
  • the difference between the heat quantity of crystallization and the heat quantity of fusion exceeds 20 J/g, the degree of crystallinity of the resin coating layer 3 is high, and the residual stress after forming is high. For this reason, appearance defects are caused by heat treatment.
  • the degree of crystallinity of the resin coating layer 3 can be controlled by controlling the degree of orientation and melting point of the resin coating layer 3 before lamination and lamination conditions (steel sheet heating temperature, nip pressure, time until water cooling after lamination, cooling temperature after lamination, and line speed). Specifically, by increasing the heating temperature of the metal sheet 2 during lamination, the degree of crystallinity of the resin coating layer 3 can be reduced.
  • the heating temperature of the metal sheet 2, which differs by the melting point and degree of crystallinity before lamination of the resin coating layer 3, is higher than the melting point of the resin coating layer 3 by 10 to 50 °C.
  • the cooling effect of the resin coating layer 3 by the nip is reduced, thereby reducing the degree of crystallinity of the resin coating layer 3.
  • the crystallization of the resin coating layer 3 during the cooling process after lamination can be reduced, thereby reducing the degree of crystallinity of the resin coating layer 3.
  • the time until water cooling after lamination which depends on a line speed, is within a range of 0.5 seconds to 10 seconds.
  • the degree of crystallinity of the resin coating layer 3 can be reduced even under the same condition as to heating roll temperature. This is because the influence of natural cooling or the like after it is heated until it is laminated diminishes.
  • the melting point of the resin coating layer 3 is within a range of 240°C or more and 254°C or less, preferably 242°C or more and 252°C or less, and more preferably 244°C or more and 250°C or less.
  • the melting point of the resin coating layer 3 is less than 240°C, the resin coating layer 3 is likely to soften through surface sliding during working, the working heat generation of the metal sheet 2, or the like, which may lead to the occurrence of a scrape on the surface of the resin coating layer 3 or the breakage thereof.
  • the melting point of the resin coating layer 3 exceeds 254°C, the degree of crystallinity of the resin coating layer 3 increases, and it may fail to allow working at a high degree of working.
  • the intrinsic viscosity (IV) of the resin coating layer 3 is within a range of 0.55 dl/g or more and 0.90 dl/g or less, preferably 0.58 dl/g or more and 0.80 dl/g or less, and more preferably 0.59 dl/g or more and 0.78 dl/g or less.
  • the intrinsic viscosity of the resin coating layer 3 is less than 0.55 dl/g, the melt viscosity of the resin coating layer 3 is low, thereby making uneven deformation of the resin coating layer 3 likely to occur during heat treatment.
  • the intrinsic viscosity of the resin coating layer 3 exceeds 0.90 dl/g, film formability degrades.
  • the intrinsic viscosity (IV) of a laminated resin can be adjusted by changes in polymerization conditions (polymerization catalyst amount, polymerization temperature, polymerization time, or the like) and the solid phase polymerization method in an inert gas atmosphere such as nitrogen or in a vacuum following melt polymerization.
  • the resin coating layer 3 is required to be white to allow treatment for improving designability such as printing treatment.
  • the resin coating layer 3 is preferable to contain titanium oxide in an amount within a range of 8 wt% or more and 30 wt% or less, preferably 10 wt% or more and 25 wt% or less, and more preferably 12 wt% or more and 20 wt% or less.
  • the content of the titanium oxide is less than 8 wt%, sufficient whiteness cannot be ensured after working.
  • the content of the titanium oxide exceeds 30 wt%, forming at a high degree of working causes problems with the adhesion between the metal sheet 2 and the resin coating layer 3 and workability.
  • titanium oxide added to the resin coating layer 3 which is not limited in particular, one whose purity of rutile type titanium oxide is 90% or more is preferably used.
  • the purity of rutile type titanium oxide is less than 90%, the dispersibility of titanium oxide is poor when it is mixed with the resin material, which may result in a reduced molecular weight of the resin material.
  • a method for adding titanium oxide may use various methods listed in (1) to (2) below. When adding titanium oxide using the method (1), titanium oxide is preferably added to a reaction system as slurry dispersed in glycol.
  • the thickness of the resin coating layer 3 with titanium oxide added is preferable to be within a range of 10 to 40 ⁇ m, preferably 12 to 35 ⁇ m, and more preferably 15 to 25 ⁇ m to ensure the whiteness of the degree of working.
  • the thickness of the resin coating layer 3 is less than 10 ⁇ m, cracking is likely to develop in the resin coating layer 3 during working.
  • the thickness of the resin coating layer 3 exceeding 40 ⁇ m gives excessive quality, which is uneconomical.
  • the resin coating layer 3 may have a three-layer structure of an outermost layer (an upper layer) 3a, an intermediate layer 3b, and a lowermost layer (a lower layer) 3c.
  • the film thickness of the outermost layer 3a and the lowermost layer 3c may be within a range of 1 ⁇ m or more and 5 ⁇ m or less, preferably 1.5 ⁇ m or more and 4 ⁇ m or less, and more preferably 2 ⁇ m or more and 3 ⁇ m or less
  • the film thickness 3c of the intermediate layer may be within a range of 6 ⁇ m or more and 30 ⁇ m or less, preferably 8 ⁇ m or more and 25 ⁇ m or less, and more preferably 10 ⁇ m or more and 20 ⁇ m or less.
  • the outermost layer 3a and the lowermost layer 3c may contain titanium oxide in an amount within a range of 0 wt% or more and 2 wt% or less, and the intermediate layer 3b may contain titanium oxide in an amount within a range of 10 wt% or more and 30 wt% or less.
  • the film thickness of the outermost layer 3a and the lowermost layer 3c is less than 1 ⁇ m, a scrape develops in the resin coating layer 3, or the luster of the surface of the resin coating layer 3 cannot be ensured sufficiently.
  • the film thickness of the outermost layer 3a and the lowermost layer 3c exceeds 5 ⁇ m, it is required to increase the film thickness of the intermediate layer 3b containing titanium oxide or increase the content of titanium oxide to ensure the whiteness, which is unfavorable in economy and workability.
  • the difference in the melting points among the outermost layer 3a, the intermediate layer 3b, and the lowermost layer 3c is 10°C or less, preferably 6°C or less, and more preferably 3°C or less.
  • a wax component may be applied or added to the resin coating layer 3.
  • the wax component to be applied or added which is not limited in particular, organic lubricants and inorganic lubricants can be applied.
  • the wax component preferably used are aliphatic waxes having a melting point of 30°C or more such as straight-chain aliphatic series such as paraffin and fatty acid esters.
  • fatty acids and fatty acid esters such as stearic acid, stearate, palmitic acid, and palmitate, which are favorable in compatibility with a polyester resin.
  • the application amount of the wax component is preferably within a range of 20 to 80 mg/m 2 .
  • the lubricating effect reduces, which is unfavorable.
  • the application amount of the wax component exceeds 80 mg/m 2 , the wax component is excessive, and the wax component remains as a solid content in a mold in the manufacture of cans, thereby inhibiting can manufacturability.
  • the addition amount of the wax component is preferably within a range of 0.01 wt% to 5 wt%. When the addition amount of the wax component is less than 0.01 wt%, the lubricating effect reduces, which is unfavorable.
  • the addition amount of the wax component exceeds 5 wt%, transfer of the wax component or the like occurs when the resin coating layer 3 is wound in a roll shape, which will be problematic.
  • the resin coating layer 4 is preferably formed of a resin material whose difference between the heat quantity of crystallization and the heat quantity of fusion after being laminated to the metal sheet 2 is within a range of 0 J/g or more and 10 J/g or less on a unit weight basis.
  • the resin coating layer 4 is in an amorphous state, the degree of crystallinity of the resin coating layer 4 is nearly zero, and a residual stress after forming also reduces.
  • the difference between the heat quantity of crystallization and the heat quantity of fusion exceeds 10 J/g, the degree of crystallinity of the resin coating layer 4 is high, and the residual stress after forming is high.
  • the degree of crystallinity of the resin coating layer 4, in the same manner as the crystallinity of the resin coating layer 3, can be controlled by controlling the degree of orientation and melting point of the resin coating layer 4 before lamination and lamination conditions (temperature, nip pressure, and cooling time and temperature).
  • the resin coating layer 4 is preferably formed of a resin material having a melting point lower than the melting point of the resin coating layer 3 by a range of 4°C or more and 20°C or less, preferably 6°C or more and 14°C or less.
  • the resin coating layer 4 does not melt sufficiently through heat treatment after working, thereby resulting in imperfect repair of minute physical flaws or the like along with working.
  • the resin coating layer 4 melts excessively through heat treatment after working, causing thermal degradation to impair laminatability.
  • the resin coating layers of Examples 1 to 23 and Comparative Examples 1 to 10 listed in Tables 1 to 3 below were formed on both sides of the metal sheet using the film laminate method (the film thermocompression bonding method). Specifically, with the metal sheet heated to a temperature higher than the melting point of the resin coating layer by 20°C, the film-shaped resin coating layer prepared by the biaxial drawing method using nip rolls was thermocompressed onto the metal sheet and then cooled through water cooling of 5 seconds or less, thereby applying the resin coating layers to both sides of the metal sheet.
  • a resin coating layer (an outer resin layer) containing a white pigment was laminated to the front side of the metal sheet positioned outside a container after forming, and a resin coating layer (an inner resin layer) containing no white pigment was laminated to the back side of the metal sheet positioned inside the container.
  • a resin coating layer an inner resin layer containing no white pigment was laminated to the back side of the metal sheet positioned inside the container.
  • For the outer resin layer its whiteness was measured. The measurement results are listed in Tables 1 to 3 below.
  • the resin coating layer was removed from the resin coated metal sheet with diluted hydrochloric acid, and washed sufficiently with distilled water to dry. Using a differential scanning calorimetry apparatus, measured was an exothermic peak and an endothermic peak when the temperature of the resin coating layer was raised from - 50°C to 290°C at a rate of temperature rise of 10°C/min.
  • the heat quantity of crystallization was calculated from the area of the exothermic peak measured in a range of 100 to 200°C
  • the heat quantity of fusion was calculated from the area of the endothermic peak measured in a range of 200 to 280°C.
  • the outer resin layer with a weight excluding the content of titanium oxide as a resin amount, the heat quantity of crystallization and the heat quantity of fusion per unit resin weight were calculated.
  • the whiteness of the resin coating layer 3 of the resin coated metal sheet was evaluated by the method listed in JIS Z8722.
  • the L-value of the Hunter Lab values measured under observation conditions with a measurement area of 30 mm dia., a measurement light source of C condition, and a field of view of 2° with respect to the measurement light source was determined to be the whiteness.
  • the outer resin layer is formed of a resin material whose difference between the heat quantity of crystallization and the heat quantity of fusion is 20 J/g or less on a unit weight basis.
  • the outer resin layer is formed of a resin material whose difference between the heat quantity of crystallization and the heat quantity of fusion exceeds 20 J/g on a unit weight basis.
  • the resin coating layer of the can flange part of the deep drawn can on which heat treatment was performed in the surface roughness evaluation was scraped to expose the metal sheet.
  • a 5% saline solution was then injected into the can, and a platinum electrode was immersed into this (the immersing position was at the central part of the can).
  • a voltage of 6 V was applied between the electrodes, and a current value was read after a lapse of 4 seconds.
  • An average value of the current values after performing measurement for 10 cans was determined to give grades in accordance with the standards listed below.
  • a sample for a peel test (15 mm wide ⁇ 120 mm long) was cut out from the can barrel part of the deep drawn can formed in the surface roughness evaluation.
  • the resin coating layer was partially peeled off from the long-side edge of the cut-out sample.
  • the peeled resin coating layer was opened in a direction (at an angle of 180 degrees) opposite the metal sheet from which the resin coating layer was peeled off, and the peel test was performed with a tensile speed of 30 mm/min to evaluate adhesion per a width of 15 mm in accordance with the standards listed below.
  • the surface for which adhesion was measured was on the inside of the can.
  • the whiteness (L-value) of the resin lamination layer 3 after resin lamination was measured to evaluate whiteness.
  • the present invention can provide a resin coated metal sheet in which no appearance defect is caused by heat treatment.
EP11871436.9A 2011-08-31 2011-08-31 Tôle métallique revêtue de résine Active EP2752291B1 (fr)

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EP3616904A4 (fr) * 2017-05-31 2020-05-06 JFE Steel Corporation Plaque métallique revêtue de résine pour récipient
EP3725512A4 (fr) * 2017-12-15 2021-08-11 JFE Steel Corporation Plaque métallique revêtue de résine pour récipients

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EP3278980A4 (fr) * 2015-03-31 2018-12-05 JFE Steel Corporation Plaque métallique stratifiée pour récipient
US10427381B2 (en) 2015-03-31 2019-10-01 Jfe Steel Corporation Laminated metal sheet for container
EP3616904A4 (fr) * 2017-05-31 2020-05-06 JFE Steel Corporation Plaque métallique revêtue de résine pour récipient
US11401092B2 (en) 2017-05-31 2022-08-02 Jfe Steel Corporation Resin-coated metal sheet for container
EP3725512A4 (fr) * 2017-12-15 2021-08-11 JFE Steel Corporation Plaque métallique revêtue de résine pour récipients
US11407203B2 (en) 2017-12-15 2022-08-09 Jfe Steel Corporation Resin-coated metal sheet for container

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EP2752291B1 (fr) 2023-09-27
MY165001A (en) 2018-02-28
EP2752291A4 (fr) 2015-03-11
CN103781626B (zh) 2016-08-31
WO2013030972A1 (fr) 2013-03-07
CA2845765C (fr) 2016-06-14
CA2845765A1 (fr) 2013-03-07
JP5733405B2 (ja) 2015-06-10
US9506152B2 (en) 2016-11-29
US20140162055A1 (en) 2014-06-12
JPWO2013030972A1 (ja) 2015-03-23
CN103781626A (zh) 2014-05-07

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